Books on the topic 'Stiffened structures'

Kolisnik, Henry M. A survey of methods of analysis for stiffened shell structures. Kingston, Ont., Canada: Dept. of Civil Engineering, Royal Military College, 1985.

Driscoll, Jennifer Culbertson. Crushing characteristics of web girders in unidirectionally stiffened double hull structures. Springfield, Va: Available from the National Technical Information Service, 1992.

Daniels, H. A. M. A CAD-system for the design of stiffened panels in wing box structures. Amsterdam: National Aerospace Laboratory, 1985.

Simitses, George J. Buckling of delaminated long panels under pressure and of radially-loaded stiffened annular plates. Atlanta, Ga: Georgia Institute of Technology, 1985.

Munroe, J. Integral airframe structures (IAS): Validated feasibility study of integrally stiffened metallic fuselage panels for reducing manufacturing costs. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 2000.

Ko, William L. Thermal and mechanical buckling analysis of hypersonic aircraft hat-stiffened panels with varying face sheet geometry and fiber orientation. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1996.

Hales, Stephen J. Structure-property correlations in Al-Li alloy integrally stiffened extrusions. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 2001.

Danielson, D. A. Tripping of stiffened plates using a refined beam theory. Monterey, Calif: Naval Postgraduate School, 1988.

L, Phillips John. Structural analysis and optimum design of geodesically stiffened composite panels. Blacksburg, Va: Virginia Polytechnic Institute and State University, Center for Composite Materials and Structures, 1990.

Nast, Trina E. Cyclic behavior of stiffened gusset plate-brace member assemblies. Edmonton: Dept. of Civil and Environmental Engineering, University of Alberta, 1999.

Castillo, Henry A. Optimum design of isotropic monocoque and ring-stiffened circular cylindrical shells subject to external hydrostatic pressure. Monterey, California: Naval Postgraduate School, 1992.

Stroud, W. Jefferson. Effect of bow-type initial imperfection on reliability of minimum-weight, stiffened structural panels. Hampton, Va: Langley Research Center, 1993.

Ryaboy, V. M. A simple model of a stiffened shell type structure for an investigation into the vibration-buckling correlation. Haifa, Israel: Technion Israel Institute of Technology, Faculty of Aerospace Engineering, 1994.

Beiter, Keith A. The effect of stiffener smearing in a ship-like box structure subjected to an underwater explosion. Monterey, Calif: Naval Postgraduate School, 1998.

Slater, J. E. Air-blast loading and structural response of a ship stiffened panel in a re-entrant corner at event "misty picture". Ralston, Alta: Defence Research Establishement Suffield, 1993.

Engineers, Institution of Mechanical, and Institution of Mechanical Engineers. Aerospace Industries Division., eds. Designing high-performance stiffened structures. Bury St Edmunds: Professional Engineering Publications for The Institution of Mechanical Engineers, 2000.

IMechE (Institution of Mechanical Engineers). Designing High Performance Stiffened Structures (Imeche Seminar Publication). Wiley, 2000.

Formulation of an improved smeared stiffener theory for buckling analysis of grid-stiffened composite panels. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., ed. Abrasion behavior of aluminum and composite skin coupons, stiffened skins, and stiffened panels representative of transport airplane structures. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.

Design and evaluation of a foam-filled hat-stiffened panel concept for aircraft primary structural applications. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.

W, Hyer M., and United States. National Aeronautics and Space Administration., eds. Calculation of skin-stiffener interface stresses in stiffened composite panels. Blacksburg, Virginia: College of Engineering, Virginia Polytechnic Institute and State University, 1987.

W, Hyer M., and United States. National Aeronautics and Space Administration, eds. Calculation of skin-stiffener interface stresses in stiffened composite panels. Blacksburg, Virginia: College of Engineering, Virginia Polytechnic Institute and State University, 1987.

W, Hyer M., and United States. National Aeronautics and Space Administration, eds. Calculation of skin-stiffener interface stresses in stiffened composite panels. Blacksburg, Virginia: College of Engineering, Virginia Polytechnic Institute and State University, 1987.

Calculation of skin-stiffener interface stresses in stiffened composite panels. Blacksburg, Virginia: College of Engineering, Virginia Polytechnic Institute and State University, 1987.

Calculation of skin-stiffener interface stresses in stiffened composite panels. Blacksburg, Virginia: College of Engineering, Virginia Polytechnic Institute and State University, 1987.

Structural analysis and design of geodesically stiffened composte panels with variable stiffener distribution. [Washington, DC: National Aeronautics and Space Administration, 1992.

F, Card Michael, and United States. National Aeronautics and Space Administration., eds. Effects of stiffening and mechanical load on thermal buckling of stiffened cylindrical shells: Presented at the AIAA/ASCE/ASC 36th Structures, Structural Dynamics and Materials Conference, April 10-12, 1995, New Orleans, LA, Thermal Structures Category. [Washington, D.C: National Aeronautics and Space Administration, 1995.

F, Card Michael, and United States. National Aeronautics and Space Administration., eds. Effects of stiffening and mechanical load on thermal buckling of stiffened cylindrical shells: Presented at the AIAA/ASCE/ASC 36th Structures, Structural Dynamics and Materials Conference, April 10-12, 1995, New Orleans, LA, Thermal Structures Category. [Washington, D.C: National Aeronautics and Space Administration, 1995.

Damping in Stiffener Welded Structures. Storming Media, 2003.

Jefferson, Stroud W., and Langley Research Center, eds. Reliability of stiffened structural panels: two examples. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.

Structure-property correlations in Al-Li alloy integrally stiffened extrusions. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 2001.

Structure-property correlations in Al-Li alloy integrally stiffened extrusions. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 2001.

A, Hafley Robert, and Langley Research Center, eds. Structure-property correlations in Al-Li alloy integrally stiffened extrusions. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 2001.

Chauncey, Wu K., Robinson James C, and Langley Research Center, eds. Analytical comparison of three stiffened panel concepts. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.

Analytical comparison of three stiffened panel concepts. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.

R, Seshadri B., and Langley Research Center, eds. Fracture analysis of the FAA/NASA wide stiffened panels. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.

R, Ambur Damodar, and United States. National Aeronautics and Space Administration., eds. Response of composite panels with stiffness gradients due to stiffener terminations and cutouts. [Washington, D.C: National Aeronautics and Space Administration, 1997.

George C. Marshall Space Flight Center., ed. AFT segment dome-to-stiffener factory joint insulation void elimination: Final report. Brigham, UT: Thiokol Corp., Space Operations, 1991.

George C. Marshall Space Flight Center., ed. AFT segment dome-to-stiffener factory joint insulation void elimination: Final report. Brigham, UT: Thiokol Corp., Space Operations, 1991.

Jefferson, Stroud W., and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Effect of bow-type initial imperfection on reliability of minimum-weight, stiffened structural panels. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.

Jefferson, Stroud W., and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Effect of bow-type initial imperfection on reliability of minimum-weight, stiffened structural panels. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.

Center, Langley Research, ed. Design and evaluation of a foam-filled hat-stiffened panel concept for aircraft primary structural applications. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.

R, Johnson Eric, and United States. National Aeronautics and Space Administration., eds. Influence of an asymmetric ring on the modeling of an orthogonally stiffened cylindrical shell. Blacksburg, Va: Virginia Polytechnic Institute and State University, 1994.

The Effect of Stiffener Smearing in a Ship-Like Box Structure Subjected to an Underwater Explosion. Storming Media, 1998.

Center, Langley Research, ed. Effect of debond growth on stress-intensity factors in a cracked orthotropic sheet stiffened by a semi-infinite orthotropic sheet. Washington, D.C: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.